Predictor LOS-based trajectory linearization control for path following of underactuated unmanned surface vehicle with input saturation

被引:38
|
作者
Qiu, Bingbing [1 ]
Wang, Guofeng [1 ]
Fan, Yunsheng [1 ]
机构
[1] Dalian Maritime Univ, Marine Elect Engn Coll, Dalian 116026, Peoples R China
基金
中国国家自然科学基金;
关键词
Unmanned surface vehicle; Path following; Line-of-sight; Trajectory linearization control technology; Minimal learning parameter; Finite-time nonlinear tracking differentiator; HYPERSONIC REENTRY VEHICLE; TRACKING CONTROL; NONLINEAR-SYSTEMS; AERIAL VEHICLES; GUIDANCE; VESSELS;
D O I
10.1016/j.oceaneng.2020.107874
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
This paper investigates a novel robust path following control scheme for unmanned surface vehicle (USV) with unknown dynamics, currents and actuator saturation. In the guidance loop, an improved predictor line-of-sight (PLOS) guidance law is presented, which is used in any parametric paths. In the control loop, we propose a yaw rate controller and a surge speed controller using trajectory linearization control (TLC) technology, finite-time nonlinear tracking differentiator (FTNTD), minimal learning parameter (MLP) technique and auxiliary system. The advantages of the developed scheme are that, first, the proposed PLOS provides the estimates of unknown sideslip angle and currents; second, the introduced TLC has a concise structure and strong robustness, and enhanced TLC only needs two parameters to be adjusted. A MLP technique is constructed to approximate lumped unknown dynamics, where the norm of all the weights is estimated instead of estimating each element to reduce computational burden. A FTNTD is concurrently used to achieve satisfactory differential and filter performance. Subsequently, a smooth auxiliary system is applied to handle input saturation constraint on actuator. Theoretical analysis illuminates that the system is semi-globally uniformly ultimately bounded (SGUBB). The effectiveness of the developed scheme is verified by simulation comparison and the error quantification performance.
引用
收藏
页数:12
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